In-flight reconfigurable aircraft tail
First Claim
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1. A system for a reconfigurable aircraft, comprising:
- a fuselage having one or more propellers;
a first tail assembly comprising a first portion that is coupled to a second portion;
a second tail assembly comprising a third portion that is coupled to a fourth portion;
a processor; and
a memory having instructions stored thereon that, when executed by the processor, cause the system to;
determine a safety clearance for the first tail assembly and the second tail assembly;
selectively move the first tail assembly upon a determination that the safety clearance is achieved by selectively moving the second portion between a retracted position relative to the first portion and an extended position relative to the first portion; and
selectively move the second tail assembly upon a determination that the safety clearance is achieved by selectively moving the fourth portion between a retracted position relative to the third portion and an extended position relative to the third portion,wherein the second portion rotates towards the fourth portion and the fourth portion rotates towards the second portion when selectively moving the second portion and the fourth portion from the extended position to the retracted position.
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Abstract
A system and method for a reconfigurable aircraft having a fuselage with one or more propellers, at least one tail assembly, a processor, and a memory having instructions stored thereon that, when executed by the processor, cause the system to: determine a safety clearance for the at least one tail assembly; and selectively move the at least one tail assembly upon a determination that the safety clearance is achieved.
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Citations
14 Claims
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1. A system for a reconfigurable aircraft, comprising:
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a fuselage having one or more propellers; a first tail assembly comprising a first portion that is coupled to a second portion; a second tail assembly comprising a third portion that is coupled to a fourth portion; a processor; and a memory having instructions stored thereon that, when executed by the processor, cause the system to; determine a safety clearance for the first tail assembly and the second tail assembly; selectively move the first tail assembly upon a determination that the safety clearance is achieved by selectively moving the second portion between a retracted position relative to the first portion and an extended position relative to the first portion; and selectively move the second tail assembly upon a determination that the safety clearance is achieved by selectively moving the fourth portion between a retracted position relative to the third portion and an extended position relative to the third portion, wherein the second portion rotates towards the fourth portion and the fourth portion rotates towards the second portion when selectively moving the second portion and the fourth portion from the extended position to the retracted position. - View Dependent Claims (2, 3, 4, 5, 12, 13, 14)
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6. A method for controlling a reconfigurable aircraft, comprising:
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receiving, with a processor, one or more signals indicative of position of the aircraft with the ground; determining, with the processor, information indicative of a safety clearance for a first tail assembly comprising a first portion that is coupled to a second portion and a second tail assembly comprising a third portion that is coupled to a fourth portion; selectively moving the first tail assembly upon a determination that the safety clearance is achieved by selectively moving the second portion between a retracted position relative to the first portion and an extended position relative to the first portion; and selectively moving the second tail assembly upon a determination that the safety clearance is achieved by selectively moving the fourth portion between a retracted position relative to the third portion and an extended position relative to the third portion, wherein the second portion rotates towards the fourth portion and the fourth portion rotates towards the second portion when selectively moving the second portion and the fourth portion from the extended position to the retracted position. - View Dependent Claims (7, 8, 9, 10, 11)
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Specification